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Attitude and Vibration Control for a Flexible Spacecraft With Double-Gimbal Variable-Speed Control Moment Gyros
By: Takahiro Sasaki, Takashi Shimomura, Sam Pullen and Hanspeter Schaub.
Pub. 2018, 20pgs.
PDF File. AAS 17-853.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Observer/Kalman Filter Indentification By A Kalman Filter Of A Kalman Filter
By: Minh Q. Phan, Francesco Vicario, Richard W. Longman and Raimondo Betti .
Pub. 2017, 15pgs.
PDF File. AAS 17-201.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Converting A State-Space Model To Physical Coordinates Without A Full Set OF Sensors A Kronecker Based Method
By: Dong-Huei Tseng, Minh Q. Phan, and Richard W. Longman.
Pub. 2017, 20pgs.
PDF File. AAS 17-205.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

A Novel Vibration Damper For Small Spacecraft With Large Flexible Appendages
By: Robert Waelchli and Dongeun Seo.
Pub. 2017, 15pgs.
PDF File. AAS 17-301.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Dynamic Analysis of the Tether Transportation System Using Absolute Nodal Coordinate Formulation
By: Xin Sun, Rui Zhong, and Shijie Xu.
Pub. 2017, 20pgs.
PDF File. AAS 17-345.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Satleash - Parabolic Flight Validation of Tethered-Tugs Dynamics and Control For Reliable Space Transportation Applications
By: Vicenzo Pesce, Andrea Bellanca, Michele Lavagna, Riccardo Benvenuto, Paolo Lunghi, and Simone Rafano Carna.
Pub. 2017, 18pgs.
PDF File. AAS 17-455.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

In-Orbit Tracking of High Area to Mass Ratio Space Objective
By: Daniel N. Brack and Pini Gurfil.
Pub. 2017, 15pgs.
PDF File. AAS 17-215.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Relative-Motion Approach for Differential Correction in Orbit Determination
By: Andrew J. Sinclair, T. Alan Lovell, Kenneth Horneman, Andrew Harris and Alex Sizemore.
Pub. 2017, 12pgs.
PDF File. AAS 17-327.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Dempster-Shafer Theory Applied to Admissible Regions
By: Johnny L. Worthy III and Marcus J. Hoizinger.
Pub. 2017, 19pgs.
PDF File. AAS 17-382.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

Fuzzy Switch-Gain sliding Mode Control for SpacecraftCombined attitude and Sun Tracking System
By: Yew-Chung Chak and Renuganth Varatharajoo.
Pub. 2018, 20pgs.
PDF File. AAS 17-852.
Price: $29.00

This item is an electronic document and will be delivered by email to the address you provide within two business days.

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